Casualties unknown

Airplane Breaks Up During Nighttime Flight After Pilot Reports Fatigue (N5856C)

Chambers, AZ, US

On June 30, 2002, a Beech C35 (registration N5856C) operated by William C. Wood was involved in an aviation accident near Chambers, AZ. Investigators recorded the probable cause as: The pilot's loss of airplane control after falling asleep due to fatigue, which resulted in a structural failure of the airframe during a high speed descent after the design stress limits of the aircraft were exceeded. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

An airplane broke up during a steep high-speed descent after the pilot, who had flown 7.4 hours fighting wildfires, expressed fatigue and made arithmetic errors. The wreckage was scattered over a 1,650-foot path.

Accident Overview

During a nighttime cross-country flight in clear visual meteorological conditions, the airplane departed from controlled flight and broke up during a steep high-speed descent. Wreckage was located over a 1,650-foot-long southerly path about 0.4 miles from the last recorded radar position, with the right wing and right stabilator found early in the debris field.

Pilot Activity and Fatigue

The pilot had awakened at 0600 and reported for work at 0750. He flew five contract flights dispersing fire retardant chemical on wildfires, accumulating 7.4 flight hours on the day of the accident. Upon completing his last flight about 1900, the pilot was overheard stating "we had a tough one today." He then laid his head down on the airplane's wing and said, "dang I'm tired." A second associate reported that the pilot had experienced difficulty completing the required end-of-day paperwork, making arithmetic errors during simple addition calculations. This associate thought the pilot was tired and "mentally exhausted."

Flight Sequence

The pilot told the associate that he was going to spend the night in a local hotel, but instead departed about 2022. He requested and received VFR radar flight following service, and at no time did the pilot indicate he was experiencing any difficulties or request assistance. After about an hour of cruise flight at 10,500 feet, during the last 19 seconds of radar-recorded flight, the airplane's average ground track changed from 241 degrees to 170 degrees, while its altitude increased from 10,900 to 11,000 feet. There were no further altitude readouts. The airplane broke apart in flight and impacted flat, desert terrain at an altitude of about 6,200 feet mean sea level.

Structural Findings

The right wing spar fractures were positive overload failures, and evidence shows that the right wing separated and impacted the right stabilizer, which also then separated.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020715X01133. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.